Per
https://www.sonexaircraft.com/engines/engines.html"Sonex Aircraft engine installations must not exceed 200 lbs total weight forward of the firewall. Any builder considering use of a heavier installation should take notice of the important information contained in our Gross Weight Advisory (LSA Compliance and Safety) Letter."
One thing to keep in mind from an engineering standpoint (even though I'm no engineer) is the tail-down force required to lift a forward CG. By loading a heavier engine, you are also increasing the necessary tail-down force, and both downward forces together must be carried by the wing. Also, just how much weight can the engine mount/attach points handle at +6 G's? I don't plan on finding out, personally!
However, it does seem that the hard-line of 200lbs has more to do, specifically, with LSA rules. The following quote is in reference to max gross weight:
"Any Sonex Aircraft licensed above those limits is not Light Sport (LSA) compliant as the
wing loading exceeds the allowable wing loading for a Light Sport aircraft."